A steam turbine (10) having an inner casing (11), in which a rotor (12) that can rotate about an axis (13) is arranged, a steam passage (14) being formed between the rotor (12) and the inner casing (11), in which steam passage there is a multi-stage arrangement of guide vanes (16) secured to the inner casing (12) and rotor blades (17) secured to the rotor (12), in which arrangement hot steam coming from an inlet (15) undergoes work-performing expansion. In a steam turbine of this type, the thermal loading of the rotor and/or inner casing, in particular when starting up, is reduced by virtue of the fact that at least in the steam passage (14) plate-like protective shields (18, 19, 20), which protect the surface of the rotor (12) or inner casing (11) beneath them from the direct action of the hot steam flowing through the steam passage (14), are arranged parallel and close to the surface of the rotor (12) and/or parallel and close to the inner surface of the inner casing (11).
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11. A steam turbine comprising:
an inner casing;
a rotor that can rotate about an axis, arranged within the inner casing;
a steam passage formed between the rotor and the inner casing;
a multi-stage arrangement of guide vanes secured to the inner casing and rotor blades secured to the rotor, the multi-stage arrangement positioned in the steam passage;
a hot steam inlet, wherein when hot steam issues from the inlet, the hot steam undergoes work-performing expansion in said multi-stage arrangement; and
plate-like protective shields positioned at least in the steam passage configured and arranged to protect the surface of the rotor over the entire rotor surface between the rotor blades or the inner casing beneath said plate-like protective shields from direct action of hot steam when flowing though the steam passage, the plate-like protective shields being arranged parallel to and directly on the surface of the rotor over the entire space between the rotor blades, parallel to and directly on the inner surface of the inner casing, or both.
16. A steam turbine comprising:
an inner casing;
a rotor that can rotate about an axis, arranged within the inner casing;
a steam passage formed between the rotor and the inner casing;
a multi-stage arrangement of guide vanes secured to the inner casing and rotor blades secured to the rotor, the multi-stage arrangement positioned in the steam passage;
a hot steam inlet, wherein when hot steam issues from the inlet, the hot steam undergoes work-performing expansion in said multi-stage arrangement;
plate-like protective shields positioned at least in the steam passage configured and arranged to protect the surface of the rotor or the inner casing beneath said plate-like protective shields from direct action of hot steam when flowing though the steam passage, the plate-like protective shields being arranged parallel and close to the surface of the rotor, parallel and close to the inner surface of the inner casing, or both, said plate-like protective shields being separate from said guide vanes and rotor blades;
an intermediate space between the shields and the rotor, between the shields and the inner casing, or both, allowing cooling steam to pass.
15. A steam turbine comprising:
an inner casing;
a rotor that can rotate about an axis, arranged within the inner casing;
a steam passage formed between the rotor and the inner casing;
a multi-stage arrangement of guide vanes secured to the inner casing and rotor blades secured to the rotor, the multi-stage arrangement positioned in the steam passage;
a hot steam inlet, wherein when hot steam issues from the inlet, the hot steam undergoes work-performing expansion in said multi-stage arrangement;
plate-like protective shields positioned at least in the steam passage configured and arranged to protect the surface of the rotor or the inner casing beneath said plate-like protective shields from direct action of hot steam when flowing though the steam passage, the plate-like protective shields being arranged parallel and close to the surface of the rotor, parallel and close to the inner surface of the inner casing, or both, said plate-like protective shields being separate from said guide vanes and rotor blades;
a shaft seal between the rotor and the inner casing; and
wherein the shields comprise at least one shield positioned in the shaft seal and including an axial bore for cooling steam to pass though.
18.
A steam turbine comprising:
an inner casing;
a rotor that can rotate about an axis, arranged within the inner casing;
a steam passage formed between the rotor and the inner casing;
a multi-stage arrangement of guide vanes secured to the inner casing and rotor blades secured to the rotor, the multi-stage arrangement positioned in the steam passage;
a hot steam inlet, wherein when hot steam issues from the inlet, the hot steam undergoes work-performing expansion in said multi-stage arrangement;
plate-like protective shields positioned at least in the steam passage configured and arranged to protect the surface of the rotor beneath said plate-like protective shields from direct action of hot steam when flowing though the steam passage, the plate-like protective shields being arranged parallel and close to the surface of the rotor, said plate-like protective shields being separate from said guide vanes and rotor blades;
a shaft seal between the rotor and the inner casing; and
wherein the shields comprise at least one shield positioned in the shaft seal with a narrow gap between the at least one shield and the rotor, the narrow gap configured and arranged to reduce heat transfer from the at least one shield to the rotor.
14. A steam turbine comprising:
an inner casing;
a rotor that can rotate about an axis, arranged within the inner casing;
a steam passage formed between the rotor and the inner casing;
a multi-stage arrangement of guide vanes secured to the inner casing and rotor blades secured to the rotor, the multi-stage arrangement positioned in the steam passage;
a hot steam inlet, wherein when hot steam issues from the inlet, the hot steam undergoes work-performing expansion in said multi-stage arrangement;
plate-like protective shields positioned at least in the steam passage configured and arranged to protect the surface of the rotor or the inner casing beneath said plate-like protective shields from direct action of hot steam when flowing though the steam passage, the plate-like protective shields being arranged parallel and close to the surface of the rotor, parallel and close to the inner surface of the inner casing, or both, said plate-like protective shields being separate from said guide vanes and rotor blades;
an unobstructed shaft seal between the rotor and the inner casing; and
wherein the shields comprise at least one shield positioned in the shaft seal with a narrow gap between the at least one shield and the rotor, the inner casing, or both, the narrow gap configured and arranged to reduce heat transfer from the at least one shield to the rotor, to the inner casing, or to both.
17. A steam turbine comprising:
an inner casing;
a rotor that can rotate about an axis, arranged within the inner casing;
a steam passage formed between the rotor and the inner casing;
a multi-stage arrangement of guide vanes secured to the inner casing and rotor blades secured to the rotor, the multi-stage arrangement positioned in the steam passage;
a hot steam inlet, wherein when hot steam issues from the inlet, the hot steam undergoes work-performing expansion in said multi-stage arrangement;
plate-like protective shields positioned at least in the steam passage configured and arranged to protect the surface of the rotor over the entire rotor surface between the rotor blades or the inner casing beneath said plate-like protective shields from direct action of hot steam when flowing though the steam passage, the plate-like protective shields being arranged parallel to and close to the surface of the rotor over the entire space between the rotor blades, parallel to and close to the inner surface of the inner casing, or both, the plate-like protective shields comprising a part of the rotor blades secured to the rotor; and
wherein the shields comprise at least one shield positioned with a narrow gap between the at least one shield and the rotor, the inner casing, or both, the narrow gap configured and arranged to reduce heat transfer from the at least one shield to the rotor, to the inner casing, or to both.
1. A steam turbine comprising:
an inner casing;
a rotor that can rotate about an axis, arranged within the inner casing;
a steam passage formed between the rotor and the inner casing;
a multi-stage arrangement of guide vanes secured to the inner casing and rotor blades secured to the rotor, the multi-stage arrangement positioned in the steam passage;
a hot steam inlet, wherein when hot steam issues from the inlet, the hot steam undergoes work-performing expansion in said multi-stage arrangement;
plate-like protective shields positioned at least in the steam passage configured and arranged to protect the surface of the rotor or the inner casing beneath said plate-like protective shields from direct action of hot steam when flowing though the steam passage, the plate-like protective shields being arranged parallel and close to the surface of the rotor, parallel and close to the inner surface of the inner casing, or both;
wherein the protective shields are arranged at a distance from a surface to be protected of the rotor, inner casing, or both, to form an intermediate cooling space;
means for permitting cooling steam to flow though the intermediate cooling space;
wherein said protective shields comprise first protective shields arranged in front stages, as seen in the direction of flow, of the steam passage; and
means for removing cooling steam from the steam passage in one of the stages located downstream of said first protective shields and for feeding back said removed cooling steam though the intermediate cooling space in the opposite direction to the direction of flow.
2. The steam turbine as claimed in
a seal in the region of the inlet and between the rotor and the inner casing on the opposite side from the steam passage;
wherein said protective shields comprise second protective shields arranged in the region of the seal at a distance from a surface of the rotor or inner casing to be protected, so as to form a second intermediate cooling space; and
wherein when cooling steam flows though the first intermediate space behind the first protective shields, said cooling steam is then passed though said second intermediate cooling space.
3. The steam turbine as claimed in
a common intermediate space continuous though the region of the inlet, behind the first and second protective shields.
4. The steam turbine as claimed in
intermediate spaces behind the first and second protective shields connected to one another.
5. The steam turbine as claimed in
a passage routed around the region of the inlet in the inner casing and connecting together the intermediate spaces behind the first and second protective shields.
6. The steam turbine as claimed in
an outer casing;
sealing members between the outer casing and the inner casing;
a third intermediate cooling space formed by the inner casing, the outer casing, and the sealing members;
two passages;
wherein the first and second intermediate cooling spaces are connected to one another by said two passages and the third intermediate cooling space; and
wherein said two passages and the third intermediate cooling space are routed around the region of the inlet.
7. The steam turbine as claimed in
8. The steam turbine as claimed in
9. The steam turbine as claimed in
10. The steam turbine as claimed in
12. The steam turbine as claimed in
13. The steam turbine as claimed in
sealing members extending radially from the guide vanes toward the plate-like protective shields, from the plate-like protective shields toward the guide vanes, or both.
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This application is a Continuation of, and claims priority under 35 U.S.C. § 120 to, International application no. PCT/CH03/00426, filed 26 Jun. 2003, and claims priority under 35 U.S.C. § 119 to EPO patent application no. 02014534.8, filed 1 Jul. 2002, the entireties of both of which are incorporated by reference herein.
1. Field of the Invention
The present invention deals with the field of steam turbines.
2. Brief Description of the Related Art
Steam turbine rotors and inner casings, when the turbine is starting up, are subject to high thermal stresses, in particular in the region of the inlet, from the relatively hot steam flowing past them, and these stresses limit the service life of the components and the start-up time.
Therefore, various proposals have already been made in the past as to how the rotors and inner casings of steam turbines can be cooled in the critical areas without additional, external devices.
U.S. Pat. No. 4,551,063 has disclosed a medium-pressure steam turbine in which cooling steam is removed at the outlet of the high-pressure turbine prior to the reheating and is routed out of an annular space located outside the steam passage, via axial bores in the rotor, into the first two stages of the turbine, where it is fed into the steam passage from the blade roots. A solution of this type can only be employed for high-pressure turbines but not for medium-pressure turbines.
In the case of a combined high-pressure/medium-pressure steam turbine disclosed by U.S. Pat. No. 5,149,247, the stator is divided into an external stator and an internal stator, which are separated from one another by an intermediate space. For cooling purposes, cooling steam is removed from the final stage of the high-pressure part and introduced into the intermediate space. A similar solution is also disclosed in U.S. Pat. No. 6,341,937. Neither solution prevents the whole of the inner stator being exposed to the live steam.
Finally, in U.S. Pat. No. 6,010,302, the rotor is provided with a central bore through which cooling steam which has been removed at the outlet of the high-pressure stage is routed. In this solution, cooling of the inner casing is not provided and is indeed not possible.
Therefore, one aspect of the present invention includes providing a steam turbine which, with relatively simple means, allows flexible internal cooling of the rotor and/or the inner casing and thereby improves the start-up time and service life of rotor and inner casing.
One of numerous principles of the present invention concerns arranging at least in the steam passage plate-like protective shields, which protect the surface of the rotor or inner casing beneath them from the direct action of the hot steam flowing through the steam passage, the plate-like protective shield being arranged parallel and close to the surface of the rotor and/or parallel and close to the inner surface of the inner casing.
A first exemplary configuration is distinguished by the fact that the protective shields, as passive protective shields, rest directly on that surface of the rotor or the inner casing which is to be protected or are only separated from the surface to be protected by a gap. They are not actively cooled, but rather only ensure that the hot steam of the steam passage no longer flows past at a high velocity, for which reason they are referred to here as “passive” protective shields or plates. The high velocity is brought about by the rotation of the rotor and the flow of steam which is present relative to the inner casing and it intensifies the heat transfer from the hot steam to the component surface. On account of the fact that although the hot steam temperature is still active, the protective shields mean that there is no longer any relative velocity between steam and component surface, the heat transfer is significantly reduced. The protective shields may in this case be designed (on the rotor side) as part of the rotor blades secured to the rotor.
A second exemplary configuration of the invention is characterized in that the protective shields are arranged at a distance from that surface of the rotor or inner casing which is to be protected, so as to form a relatively wide intermediate space, and in that the steam turbine is designed in such a manner that cooling steam flows through the intermediate space. Exemplarily, first protective shields are arranged in the front stages, as seen in the direction of flow, of the steam passage, and the cooling steam is removed from the steam passage in one of the stages located further downstream and is fed back through the intermediate space in the opposite direction to the direction of flow.
Therefore, heated steam which is only removed from the steam passage when it has already passed through a pressure drop is used. Consequently, the steam is cooler than the steam in the inlet. This cooler steam is then diverted and passed into the intermediate spaces along the rotor surface or the casing surface to the first stages, which are acted on by the hottest steam. To ensure that the cooling or cool steam can flow in this direction, it is passed to a location at a lower pressure level. This location may, for example, be a sealing chamber in a piston or casing shaft seal or, in the case of double-flow machines, a rear stage in the second flow. However, this location may also be the exhaust steam of the machine. To ensure that no hot steam is able to flow into the cooling intermediate spaces, it is necessary for the cooling intermediate space to be sealed off with respect to the hot steam at a higher pressure. Pressure tight protective shields or plates are used for this purpose.
If in particular the steam turbine is of single-flow design, and in the region of the inlet a seal, in particular in the form of a piston or casing shaft seal, is provided between rotor and inner casing on the opposite side from the steam passage, second protective shields are arranged, for example, in the region of the seal at a distance from that surface of the rotor or inner casing which is to be protected, so as to form a relatively wide intermediate space, and the cooling steam flowing through the intermediate space behind the first protective shields is then passed through the spaces behind the second protective shields.
If in this case the first and second protective shields are intended to protect the surface of the rotor, a common intermediate space which is continuous through the region of the inlet is formed behind the first and second protective shields.
If the first and second protective shields are intended to protect the surface of the inner casing, intermediate spaces, which are connected to one another, e.g., by a passage or bore routed around the region of the inlet in the inner casing, are formed behind the first and second protective shields.
The invention is to be explained in more detail below on the basis of exemplary embodiments in conjunction with the drawing, in which:
Finally,
While the invention has been described in detail with reference to exemplary embodiments thereof, it will be apparent to one skilled in the art that various changes can be made, and equivalents employed, without departing from the scope of the invention. Each of the aforementioned documents is incorporated by reference herein in its entirety.
Patent | Priority | Assignee | Title |
10774667, | Dec 06 2013 | GE INFRASTRUCTURE TECHNOLOGY LLC | Steam turbine and methods of assembling the same |
10935007, | Feb 10 2017 | MITSUBISHI POWER, LTD | Geothermal turbine |
8221056, | Jun 11 2009 | General Electric Company | Mixing hotter steam with cooler steam for introduction into downstream turbine |
8221062, | Jan 14 2009 | GE INFRASTRUCTURE TECHNOLOGY LLC | Device and system for reducing secondary air flow in a gas turbine |
8348608, | Oct 14 2009 | General Electric Company | Turbomachine rotor cooling |
8376687, | Oct 13 2009 | General Electric Company | System and method for cooling steam turbine rotors |
8662826, | Dec 13 2010 | General Electric Company | Cooling circuit for a drum rotor |
8668439, | Mar 24 2011 | General Electric Company | Inserts for turbine cooling circuit |
8845284, | Jul 02 2010 | General Electric Company | Apparatus and system for sealing a turbine rotor |
8864453, | Jan 20 2012 | GE INFRASTRUCTURE TECHNOLOGY LLC | Near flow path seal for a turbomachine |
8992168, | Oct 28 2011 | RTX CORPORATION | Rotating vane seal with cooling air passages |
9080456, | Jan 20 2012 | GE INFRASTRUCTURE TECHNOLOGY LLC | Near flow path seal with axially flexible arms |
9228445, | Dec 23 2010 | General Electric Company | Turbine airfoil components containing ceramic-based materials and processes therefor |
9702261, | Dec 06 2013 | GE INFRASTRUCTURE TECHNOLOGY LLC | Steam turbine and methods of assembling the same |
Patent | Priority | Assignee | Title |
2552239, | |||
4405284, | May 16 1980 | MTU Motoren-und Turbinen-Union Munchen GmbH | Casing for a thermal turbomachine having a heat-insulating liner |
4551063, | Mar 18 1983 | Kraftwerke Union AG | Medium-pressure steam turbine |
5149247, | Apr 26 1989 | GEC Alsthom SA | Single HP-MP internal stator for a steam turbine with controlled steam conditioning |
5503405, | May 07 1991 | General Electric Co. | Apparatus for providing uniform radial clearance of seals between rotating and stationary components |
5524340, | Sep 13 1994 | General Electric Co.; General Electric Company | Method for modifying a turbine diaphragm for use with a reduced rotor lan diameter |
5558496, | Aug 21 1995 | General Electric Company | Removing particles from gas turbine coolant |
6010302, | Jan 11 1996 | Siemens Aktiengesellschaft | Turbine shaft of a steam turbine with internal cooling and method for cooling a turbine shaft of a steam turbine |
6045134, | Feb 04 1998 | General Electric Company | Combined labyrinth and brush seals for rotary machines |
6341937, | Nov 01 1999 | MITSUBISHI HITACHI POWER SYSTEMS, LTD | Steam turbine with an improved cooling system for the casing |
6416276, | Mar 29 1999 | ALSTOM SWITZERLAND LTD | Heat shield device in gas turbines |
6783321, | Nov 06 2002 | General Electric Company | Diffusing coupling cover for axially joined turbines |
CH308991, | |||
CH340669, | |||
DE1576975, | |||
EP1076184, | |||
FR897716, |
Executed on | Assignor | Assignee | Conveyance | Frame | Reel | Doc |
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Apr 26 2005 | REIGL, MARTIN | Alstom Technology Ltd | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 015971 | /0874 | |
Nov 02 2015 | Alstom Technology Ltd | GENERAL ELECTRIC TECHNOLOGY GMBH | CHANGE OF NAME SEE DOCUMENT FOR DETAILS | 039714 | /0578 |
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